Solutions to the Direct Problem of Heat Transfer between a Cooled Turbine Blade and Gas using the Dispersion Method,

Abstract

The dispersion method is used to solve a differential equation of the third order describing heat exchange between gas and a cooled turbine blade.

Document Details

Document Type
Technical Report
Publication Date
Jul 24, 1974
Accession Number
AD0783927

Entities

People

  • A. M. Topunov
  • N. G. Rodionov
  • R. D. Iosifov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Differential Equations
  • Dispersions
  • Energy Transfer
  • Equations
  • Heat Transfer
  • Mathematics
  • Rotor Blades (Turbomachinery)
  • Turbine Blades
  • Turbines
  • Turbomachinery

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Aerodynamics.
  • Combustion and Flow Dynamics.